Note : Les descriptions sont présentées dans la langue officielle dans laquelle elles ont été soumises.
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A MARINE PROPELLER
FIELD OF INVENTION
The present invention .r_elates to a marine propeller of the
kind defined in the preamble of Claim 1. The adjustable
blades of such propellers enable the propeller to be adapted
to different running conditions and different types of engine
or motor. One advantage with such propellers is that they
cover a wider area ~~f use than fixed blade propellers. This
enables propeller manufacturers and suppliers to satisfy the
requirements of different. users with a relatively limited
number of types of propeli.er i.n the general assortment.
BACKGROUND OF T8E INVENTION
Adjustable b~.ade propellers have = long been known. These
propellers can be divided into'two main types, one type with
which each blade can be adjusted individually, and another
type with which all. ~ladeg are adjusted commonly in one
single movement. One advantage with the latter type of
propeller is that it eliminates the need to bring the
individual setting of a blade into agreement with the
settings of the remaining blades, which can be difficult to
achieve and which may result in differences in blade
settings.
The inventive propeller :Lies within this latter type of
propeller, i.e. a propeller with which the propeller blades
can be adjusted in unison.
Adjustable blade propellers of this kind are described and
illustrated in U. S. t3I3, 0'74, U. S. 2, 574, 951, U. S. 5, 232, 345,
U.S. 2,953,208, U.S. 3,403,735, U.S. 3,308,889, for instance.
A common feature of the propeller constructions described in
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these publications is that common or unison adjustment of the
blades is made to a completely optional setting within the
limits given, i.e. the blades can be adjusted to different
settings smoothly and continuously. The blades are locked in
their new settings, subsequent to this adjustment. This
procedure has several drawbacks. Firstly, it is necessary to
be able to read or determine the blade setting, so as to
establish whether or not the blade has been adjusted to the
angle intended. There is a:~so the risk of deviation between
the blade setting intended and the blade setting achieved.
Furthermore, it is necessary to rely upon force-bound locking
of the blades when p~~acticing this continuous blade
adjustment principlE. This force-bound locking of the blades
can result i r~ a change _~~-: t:he blade setting, or may require
7.5 the application of ~.o~~:.;_ny f~m-ces of sucr great magnitude as
to cause dismantling an:i fitting operations in respect of the
adjustment more difficu:~s: to achieve and induce higher
tensions in the mater3.al. There is also the risk of a heavily
tightened locking devir..e becoming loose in the passage of
time, due to vibration ar..~.-3 cther_ forces, so as to disturb the
blade settings. P.s a rc~s~iLt, a number of the earlier
constructions have bec:c~me highly complicated.
EP 0 300 252 teaches a blade adjuster with which the blades
can be adjusted to distinct settings in unison. The
arrangement is, however, relatively complicated and involves
the conversion of a tors.ional adjustment movement to an axial
adjustment movement of a rod 'chat extends to each propeller
blade, through the medium of. nuts and spindles. The axial
movement of the rod is then converted to rotational movement
of respective blades through the medium of a pin carried by
the rod and co-acting with a guide groove or channel in the
blade root.
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svY og ~ iNV»rrrioN
Against this background, it i.s an object of the invention to
provide a propeller of the kind concerned with which the
aforesaid problems associated with known techniques in this
field have been avoided. More specifically, it is an object
of the invention to provide a propeller of simple
construction with which the blades can be adjusted to
unequivocally defined and positively retained settings.
This object has been achieved in accordance with the
invention with a propeller of the kind defined in the
preamble of Claim 1 that has the particular features set
forth in the characterising clause of said Claim.
Because the common adjustment movement is performed through
the medium of relative movement between
two elements, the
adjuster ring and the hub, which can shape-locked together
be
in predetermined distinct positions, the blades can be
adjusted to defined positions such as to eliminate the risk
of accuracy deficiency and such as to obviate the need for
measuring a precise position of adjustment
or setting. All
that is required to show to which of the predetermined
positions the adjustment relates is a simple indication
index. The shape-bound locking facility also ensures that the
blade setting will not be disturb ed and affected by
vibrations and running disturbances.
The inventive propeller
is also of simple construction and therewith relatively
inexpensive in manufacture.
According to one preferred embodiment of the invention, the
means by which the adjustment adjuster ring and the hub are
locked relative to one another in their circumferential
direction are disposed on the mutually
facing surfaces of
said adjuster ring and sa~.d hub.
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The locking elements suitably have the form of axially
extending teeth with intermediate grooves or channels on each
of the two surfaces.
The grooves and teeth have a complementary shape, so as to
engage with one another in locking the adjuster ring and the
hub together . One of said surfaces will include a plurality
of teeth and the other at least one tooth, preferably several
teeth. The teeth and the grooves ensure that the shape-bound
locking effect is ~c'ru=caved and also define the blade
settings.
According to another. ~~refer_red embodiment, the movement
transmission element that transmits rotation of the setting
J.5 adjuster ring to the propeller blades is comprised of a
plurality of arms, each of which is connected at one end to
the root of a blade anca "~:ne other end of which proj ects into
a respective recess provided in the blade setting adjuster
ring. This provides s.ir:~plu and reliable transmission of
rotation of the adjuster ring to rotation of the propeller
blades.
As a result of th.:, :;i.mple construction of the blade
adjusting mechanism, space can be provided for accommodating
exhaust passages in the t,ub. A preferred embodiment o.f the
invention thus includes such an arrangement of exhaust
passages. This facility provided by said construction is
particularly beneficial in view of the fact that the
propeller is intended for use with several different types of
drive motors.
According to one particularly beneficial embodiment of an
inventive propeller, the blades are flexible so that their
propelling behaviour will be influenced by operating or
running conditions, which is of particular importance when
the propeller blades can be adjusted in distinct steps. A
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preferred embodiment of the invention also relates to this
facility.
According to another preferred embodiment, each blade has a
weakened part that forms a fracture location. This prevents
the hub from being damaged in the event of the propeller
blades striking against ~ stone or some other object. This is
of particular importance i.n respect of an inventive
propeller, since a hub that is constructed for stepwise
adjustment of the blade settings is more sensitive to
external forces than a hub to which the blades are fixedly
connected.
These and other advant:aaeous embodiments of the inventive
propeller are set forth in the dependent Claims.
The invention will now be described in more detail with
reference to a preferred embodiment thereof and also with
reference to the accompanying drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
Fig. 1 is an exploded view of an inventive propeller.
Fig. 2 is a side view of a propeller blade of an inventive
propeller.
Fig. 3 is a sectional vi.e!a taken on the line III-III in Fig.
2.
Fig. 4 is a view seen radially inwards of the blade in Fig.
2.
Fig. 5 illustrates the hub of an inventive propeller partly
in side view and partly in axial section.
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Fig. 6 is a sectional view taken on the line VI-VI in Fig. 5.
Fig. 7 is a sectional view taken on the line VII=VII in Fig.
5.
DETAII~D DESCRIPTION Oh' .A. EREP'ERRED ED~ODIZ~NT
Fig. 1 is an exploded view of an inventive propeller assembly
which comprises a hub tt:at includes a forward hub-half 1 and
-0 a rearward hub-half ~ , a unit 3 for connection to the gear
box of a drive motor, a:~ adjustment adjuster ring 4, and four
propeller blades 5, of which only two are shown in the
Figure. Each of the two h~ab-halves 1, 2 is provided with four
semi-circular recesses 6a, 6b which are located centrally of
each other and which when assembled form circular bearings 6
for respective blades 5y. Each blade 5 has a circular base-
part or root-part 7 by mEans of which it is rotatably mounted
in one of the bearings 6. rPhe two hub-halves 1, 2 are held
together by four bolts (nom shown) drawn through holes 8, 9
in the front and rear hub-halves respectively. The hub-parts
include axially through-passing passages 10, 11 through which
motor exhaust gases can pass. The propeller is driven by a
shaft (not shown) emending from a motor, and the shaft is
drivingly connected to the hub bore 12 in the rear hub-half
2, for instance by means of a spline coupling.
The root-part 7 of each blade includes a circumferentially
extending projection 1.."s which projects out radially in
relation to the rotational axis of the blade and which coacts
with a corresponding groove or channel 14 in the hub-halves
for mounting the blades to the hub and secures the blades in
the radial direction of the propeller. A blade adjusting arm
15 is attached to the periphery of each root-part and extends
generally radially relative to the rotational axis of the
blade, i.e. extends generally in the direction of the
propeller axis. The blade setting is adjusted by applying
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torque to the arm 15. When fitted, the arm 15 extends
inwardly of the outer surface of the rear hub-half 2 and back
towards the setting adjuster ring 4. Each arm 15 has a flared
end-part 16 which, when the arm is fitted, is received in a
recess I7 on the inner surface of the adjuster ring.
In operation, the adjuster ring 4 is fitted to the rear hub-
half 2, wherewith a front annular end-surface 18 abuts a rear
end-surface 19 (obscured in Fi.g. 1) of the rear hub-half 2.
In this assembled state, the adjuster ring 4 is fastened to
the hub-half 2 by means of appropriate fasteners (not shown)
and is secured against rotation by axially extending teeth 20
and intermediate grooves 21 on the end-surface 18 of the
adjuster ring, said teeth and . grooves co-acting with
correspondingly shaped t-.Feth and grooves 23 (obstructed in
Fig. 1) on the end-surface 19 of the~rear hub-part 2.
The adjuster ring 4 can b~ loosened from the rear hub-half 2
so as to be movable axially in relation thereto, and can be
displaced slightly therefrom to a second position in which
the teeth and grooves 20, 21, 22, 23 no longer co-act with
one another. The adjuster ring 4 can be rotated relative to
the rear hub-half 2 in this position. By rotating the
adjuster ring 9 slightly and then re-fastening it to the rear
hub-half 2, the teeth and the grooves 20, 21, 22, 23 will
lock the adjuster ring in the new position. Rotation of the
adjuster ring involves moving the adjuster ring axially
through only a short distance such as to ensure that the
teeth and the grooves are out of mutual engagement. However,
the end-part 16 of respective blade setting adjusting arms 15
still protrude into the recesses 17 on the adjuster ring 4 in
this position.
Thus, rotation of the adjuster ring 4 causes each arm 15 to
rotate the root-part 7 of respective blades to a setting that
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depends on the angle through which the adjuster ring is
rotated.
The positions to which the adjuster ring of the illustrated
construction can be rotated are restricted to a number of
distinct positions determined by the pitch of the teeth 20,
22. The blade settings can thus be adjusted incrementally and
the number of setting positions is dependent on the number of
teeth on the adjustEr ring or on the rear hub-half. The
adjuster ring 4 and the rear hub-half 2 need not have the
same number of teeth. The number of rotational positions is
determined by the unit that has the most teeth.
In principle, it is con~:Pivably sufficient to provide the
described locking device with teeth on only one peripheral
part of the end-surface of the adjuster ring and the rear
hub-half respectively. However, it may be convenient to
provide corresponding pairs of engaging teeth at several
places on these surfaces, as shown at 24 and 15 in the
Figure. This arrangement: provides a more positive locking
effect.
In order to show visually the distinct rotational positions
in which the rear hub-half 2 and the adjuster ring 4 are
located, there is provided a scale 27 that includes a number
of index marks on the outer surface of the rear hub-part 2,
adjacent its end-surface 19. A setting marking 26 is provided
at a corresponding position on the outer surface of the
adjuster ring 4. The position of the setting marking 26 on
the scale 27 therewith shows the rotational position of the
blades.
Since all blades are provided with an adjusting arm 15 that
co-acts with a respective recess 17 on the adjuster ring 4,
the blades 5 will be rotated in unison as the adjuster ring 4
rotates.
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Fig. 2 illustrates in more detail the annular projections 13
and associated blade adjusting arms 15 adapted for mounting
and radially securing the root-part 7 of each blade 5.
Fig. 3 is a sectional view taken on the line III-III in Fig.
2 and shows that the root-part 7 of the blade is hollow and
includes an annular part on which the projections 13 are
provided and a dome-sizaped part 28 connected integrally with
the actual blade 5. Tr:e inner surface of the dome-shaped part
28 has a circumferentially extending groove 29 which weakens
the blade at its root and therewith functions as a fracture
location. In the event of the blade 5 striking an obstacle,
such as a stone, the blade ~~=ill fracture at the groove 29
before the force reaches the hub and damages the same. This
arrangement limits propeller damage to the blade whilst
protecting the hub. It will be borne in mind that the hub of
a propeller assembly that includes a blade setting adjusting
arrangement of this kind is more expensive and less robust
than the hub of a conventional propeller with fixed blades.
The propeller blades 5 are preferably made of a flexible
material, for instance a plastic composite. When the blade 5
has a rearwardly swept profile, the outer part of the rear
edge 30 of the blade will be urged forwards through an angle
corresponding to the angle a and reach a forwardly displaced
position indicated by the broken line in Fig. 9, therewith
reducing the pitch. This takes place when the blade is
subjected to a high load, for instance in response to
acceleration. The greater the load, the greater the reduction
in pitch, resulting in easier propulsion. There is thus
obtained in this way some sort of "automatic gear function"?
which automatically reduces the pitch when the propeller is
subjected to heavy loads, due to the flexibility of the
material.
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Fig. 5 is a cross-sectional view illustrating attachment of
the blade 5 in the circular opening 6 formed between the two
hub-parts 1, 2. The peripheral, projections 13 on the blade
root 7 co-act with grooves or channels 14 on the hub-halves,
so as to secure and rotatably mount the blade in the hub. The
end-part 16 of respective blade setting adjusting arms 15
extend into the recess 17 so as to be entrained by the
adjuster ring 4 as it rotates and therewith rotate the blade
5. The adjuster ring 4 is shown in a locked position with its
end-surface in abutment with the rear end-surface of the rear
hub-half and with the mutually co-acting teeth and grooves
(not visible in this Figure) on said surfaces in mutual
locking engagement. Also shown in the Figure are four bolts
31 which hold the hub together. When adjusting the setting of
the blades, the bolts 3? are first loosened sufficiently to
enable the adjuster ring 4 to be moved axially through a
distance required to move the teeth and the grooves out of
engagement with one another and therewith enable the adjuster
ring to be turned. Subsequent to turning the adjuster ring to
a new position, the bolts are tightened in this position and
the blade setting marking 26 is moved to another position
opposite some other marking on the scale 27. The markings 26
and 27 may have the form of a painted line or a scored line.
Figs. 6 and 7 are sectional views taken respectively along
the lines VI-VI and VII-VII in Fig. 5 and serve to further
illustrate the mutual relationship of elements significant to
blade setting adjustment. The above description made with
reference to Figs. 1 and 5 is believed to make Figs. 6 and 7
self-explanatory.
